Orbital debris impact simulation using a parallel hybrid particle-element code |
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| Authors: | Eric Fahrenthold Ravishankar Shivarama |
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| Affiliation: | Department of Mechanical Engineering, University of Texas, Austin, TX 78712, USA |
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| Abstract: | Simulations of three dimensional orbital debris impact problems, using a parallel hybrid particle-finite element code, show good agreement with experiment and good speedup in parallel computation. The simulations included single and multi-plate shields as well as aluminum and composite shielding materials, at an impact velocity of eleven kilometers per second. |
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| Keywords: | impact simulation numerical methods particle methods finite element methods |
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